SINS/BDS Integrated Navigation for Hypersonic Boost-Glide Vehicles in the Launch-Centered Inertial Frame

Table 1

Initial state of the trajectory.

Parameters	Value
Velocity	0 m/s
Latitude	34.2°
Longitude	108.9°
Height	0 m
Launch azimuth	200°
Pitch	90°
Roll	0°
Yaw	0°